Numerical investigation of effect of inlet swirl and total-pressure distortion on performance and stability of an axial transonic compressor
Crossref DOI link: https://doi.org/10.1007/s11630-016-0891-6
Published Online: 2016-11-11
Published Print: 2016-12
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Naseri, A.
Boroomand, M.
Sammak, S.
License valid from 2016-11-11
